Electromagnetic and radiation shielding using nanoforests
12225701 ยท 2025-02-11
Assignee
Inventors
- William A. Goodman (Albuquerque, NM, US)
- Mohammad Naghi Ghasemi-Nejhad (Honolulu, HI, US)
- Brenden M. Minei (Honolulu, HI, US)
- Caleb Pierick (Honolulu, HI, US)
Cpc classification
H05K9/0083
ELECTRICITY
International classification
Abstract
A lightweight radiation shielding material. A carbon nanotube forest is embedded in a matrix comprising nanoparticulates, such as nanoparticles, carbon nanotubes, or graphene nanosheets. The nanoparticulates can be low atomic number (low-Z) or high atomic number (high-Z). The matrix can be a solidified polymer, epoxy, resin, or ceramic precursor, for example silicon carbide. The radiation shield can shield an object from radio frequency interference (RFI), lightning, electromagnetic interference (EMI), an electromagnetic pulse (EMP), gamma rays, X-rays, neutrons, and/or protons. The nanoforest is disposed on a conductive base with sufficient in-plane electrical conductivity to provide an effective conductive path for currents induced by radiation absorption. The base can be a second nanoforest comprising horizontally-oriented carbon nanotubes, which makes the shield particularly lightweight, as low as 10% of the mass of aluminum that provides equivalent shielding. The base can be adhered to an object to be shielded.
Claims
1. A radiation shield comprising a nanoforest comprising vertically-oriented carbon nanotubes, the nanoforest embedded in a matrix comprising nanoparticulates; wherein the nanoforest is disposed on a base, the base comprising a second nanoforest comprising horizontally-oriented carbon nanotubes.
2. The radiation shield of claim 1 wherein the nanoparticulates are nanoparticles, carbon nanotubes, or graphene nanosheets.
3. The radiation shield of claim 1 wherein the nanoparticulates comprise one or more materials selected from the group consisting of graphene, modified graphene, functionalized graphene oxide, gold, silver, copper, aluminum, and platinum.
4. The radiation shield of claim 1 wherein the matrix comprises a solidified polymer, epoxy, resin, or ceramic precursor.
5. The radiation shield of claim 1 wherein the nanoparticulates are low atomic number (low-Z).
6. The radiation shield of claim 1 capable of shielding an object from radio frequency interference (RFI) (e.g., 5G), lightning, microwave transmissions, electromagnetic radiation, electromagnetic interference (EMI), electromagnetic pulse (EMP), High-altitude Electromagnetic Pulse (HEMP), Vertical EMP (VEMP), flash X-rays, gamma rays, X-rays, and/or neutrons.
7. The radiation shield of claim 1 comprising high atomic number (high-Z) nanoparticulates, thereby enabling the radiation shield to shield an object from protons.
8. The radiation shield of claim 1 wherein the matrix comprises a ceramic.
9. The radiation shield of claim 8 wherein the ceramic is silicon carbide.
10. The radiation shield of claim 1 wherein a concentration of nanoparticulates in the matrix is greater than approximately 3.2 wt %.
11. The radiation shield of claim 10 wherein the concentration of nanoparticulates in the matrix is greater than approximately 30 wt %.
12. The radiation shield of claim 11 wherein the concentration of nanoparticulates in the matrix is greater than or equal to approximately 60 wt %.
13. The radiation shield of claim 1 wherein the vertically-oriented carbon nanotubes are between about 25 microns and about 4 mm in length.
14. The radiation shield of claim 1 wherein the base comprises sufficient in-plane electrical conductivity to provide an effective conductive path for currents induced by radiation absorption.
15. The radiation shield of claim 1 wherein a thickness of the second nanoforest is between about 40 microns and about 70 microns.
16. The radiation shield of claim 1 wherein the base is configured to adhere to an object to be shielded.
17. The radiation shield of claim 1 comprising approximately 10% of a mass of aluminum providing equivalent shielding.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The accompanying drawings, which are incorporated into and form a part of the specification, illustrate the practice of embodiments of the present invention and, together with the description, serve to explain the principles of the invention. The drawings are only for the purpose of illustrating certain embodiments of the invention and are not to be construed as limiting the invention. In the drawings:
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DETAILED DESCRIPTION OF EMBODIMENTS OF THE INVENTION
(9) Embodiments of the present invention comprise a hierarchical, multifunctional, 3-dimensional nanocomposite with a structured 3D carbon nanotube (CNT)/graphene nanosheet (GNS) labyrinthine structure having a high shielding effectiveness (SE) suitable for shielding and radiation hardening avionics, data centers, and other high valued terrestrial or airborne electronics systems preferably from radio frequency interference (RFI) (e.g., 5G), lightning, microwave transmissions, other sources of electrical magnetic interference (EMI), electromagnetic pulse (EMP), High-altitude Electromagnetic Pulse (HEMP), Vertical EMP (VEMP), flash X-rays, and even some nuclear effects due to, for example, HEMP, gamma rays, X-rays, and neutrons.
(10) In the 3D CNT/GNS labyrinthine structure of the present invention, impinging electromagnetic (EM) waves experience multiple internal reflections, volumetrically enhancing the EM wave absorption by conversion of induced currents to heat and other mechanisms. As shown in
(11) In one embodiment an epoxy matrix comprises low-Z graphene nanosheets (GNS), preferably comprising functionalized graphene oxide (GO). The nanoresin is preferably manufactured by sonication of Jeffamine hardener with additions of highly conductive graphene, GNS, and/or graphene oxide (GO), which are then preferably combined with EPON 828, to form a composition comprising a resin having a reinforcement dispersed within, the reinforcement comprising graphene bodies, carbon nanotubes, or any combination thereof. This compositing improves structural and physical (e.g. electrical and thermal conductivity) properties isotropically, but typically to a lesser extent than the nanoforest(s).
(12) Other surfactants and solvents can be used to make hyper-loaded nanoresins (i.e. resins loaded with nanoparticulates) to turn electrical insulators into conductors better than steel. The percolation threshold (defined here as the point when the electrical conductivity reaches 0.00005 S/cm) for both CNT and GNS in preceramic polymers comprising electrically insulating silicon carbide (e.g. Starfire Systems' SMP-10) is approximately 3.2 wt %. An as-cured 60 wt % GNS nanocomposite, shown in
(13) The vertically-aligned CNT nanoforest is preferably disposed on a conductive base. The base preferably both provides sufficient conductivity in the in-plane direction to provide a conductive path for induced currents resulting from EM absorption. As shown in
(14) A preferably 3D-printed embedded RF responsive structure, or Complimentary Split-Ring Resonator (CSRR), can address problematic frequencies that are known or that are discovered during testing. For the present invention design and analysis of a CSRR using a Solidworks-COMSOL model is used to assess parameters such as transmitted frequency, antenna aperture geometry, size and scale of the CSRR for filtering frequencies (bandpass or rejection), and perimeter square, corresponding to different materials and frequency range of interest. One example is shown in
(15) The electrical conductivity of pure CNTs is 10.sup.4-10.sup.5 S/cm and 10.sup.6 S/cm for pure GNS. These values compare with pure silver, copper, and aluminum metals, which have conductivities of 6.3010.sup.5, 5.9610.sup.5, and 3.7710.sup.5 S/cm, respectively. It is known that even 4 mils of high electrical conductivity copper does not meet military requirements for >70 dB attenuation from 500 MHz-100 GHz. It is expected that the present invention will require only about 1/10 the mass of aluminum for the same shielding effectiveness. Table 1 provides some relevant materials properties.
(16) TABLE-US-00001 TABLE 1 E E/ .sub.t .sub.t/ k .sub. Room Temperature Property Modulus Stiffness Strength Strength Expansion Conductivity Conductivity Density Young's Specific Tensile Specific Thermal Thermal Electrical Units: kg/m.sup.3 GPa MPa-m.sup.3/kg Mpa MPa-m.sup.3/kg 10.sup.6/K W/m-K 10{circumflex over ()}6 S/m Preferred Value: Small Large Large Large Large Small Large Large Carbon 2100 1060 505 100000 47.62 12 3000 1 to 10 Nanotube Graphene 2100 1000 476 130000 61.90 8 3000 1 to 10 Nanosheet C/Epoxy 1600 70 44 600 0.38 2.1 150 0.03 50% Sheet Steel 7900 200 25 420 0.05 11.7 50 1.45 Aluminum: 2740 71 26 503 0.18 26 121 36.9 7075 T6 OFHC 8940 117 13 379 0.04 17 390 58 Copper
(17) With respect to EM shielding, Table 1 shows that aluminum is an excellent choice, not only for its mass and electrical conductivity but also because it is a low Z material. Using Clemson's online Shielding Effectiveness Calculator (https://cecas.clemson.edu/cvel/emc/calculators/SE_Calculator/index.html), the plane wave shielding effectiveness of various materials can be calculated using the equation:
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(19) Using properties from Table 1, the SE for 1 square foot of material (0.0929 m.sup.2) of aluminum (Al), horizontally-aligned CNTs, and GNS as a function of thickness for frequencies of 0.5 and 100 GHz can be calculated. The horizontally-aligned CNT component of the orthogonal nanoforest is preferably designed for maximum conductivity, and a thickness of about 50 microns is typical. The relative permeability of the horizontally-aligned CNT and GNS was valued as 4, and Al was 1. The SE calculation results are shown in Table 2; the SE values include both reflection and absorption components. COMSOL was used to model Al plates with 0.5, 1, and 10 mm thickness across the 0.5-100 GHz frequency spectrum for an infinite plane Floquet BC; the example COMSOL output for 0.5 mm thick Al plates is shown in
(20) TABLE-US-00002 TABLE 2 Shield Layer Low Z Thickness Low Z horizontally- Low Z (m) Aluminum aligned CNT GNS SE (dB) for 0.5 GHZ / SE (dB) for 100 GHz/Mass (kg) 50 198/1716/ 190/1773/ 465/1773/ (0.05 mm) 0.0127 0.00975 0.00975 500 1267/16659/ 1290/17730/ 3943/17730/ (0.5 mm) 0.127 0.0975 0.0975 5000 11961/166084/ 12291/172906/ 38731/546691/ (5 mm) 1.27 0.975 0.975
(21) Shielding results in the literature for carbon in the 2-18 GHz range for graphene films with a bi-continuous nanoporosity had EMI SE (SSE/t) of 50.9 dB (75,407 dB cm.sup.2/g) and 83 dB (61,630 dB cm.sup.2/g). As expected, at higher frequencies for an appreciable thickness (500 microns), the absorption losses greatly exceed the reflection loss component of the SE for all the materials. The order of magnitude higher electrical conductivity of GNS results in the highest SE, from 2.35 to 3.24 times higher than Al, depending on thickness. The horizontally-aligned CNT and GNS have a 24% lower density than Al, but GNS can be nominally the thickness for the equivalent SE, and thus only .sup.th the mass of Al. It is expected that the orthogonal nanoforest will only be 1/10.sup.th the mass of Al and will simultaneously achieve an electrical conductivity of 3000 S/cm and attenuation >70 dB across the 500 MHz-100 GHz. The channels between neighboring CNTs in the vertically-aligned CNT component of the present invention provide exposure to a vast surface area of conductive surfaces (both CNT walls and the nanoparticulates in the resin matrix) in 3-dimensions, increasing internal reflections of EM waves and volumetrically enhancing the EM wave absorption by converting induced currents to heat, dielectric relaxation, and tunneling currents. One or more CSRRs, preferably 3D-printed on the composite, may be used to clean up leakage.
(22) There are many possibilities for original, EMI/EMP dedicated electronics packaging designs using the EMI/EMP shields of the present invention. Native orthogonal nanoforest/GNS nanoparticulate composite panels containing bonded-in, CTE-matched (titanium, Invar, Kovar) mounting, fastening and structural features can support a variety of internal components and configurations. A Faraday-caged avionics package will comply with full-spectrum EMI and EMC-TEMPEST environmental requirements, using EMI-filtered interconnects (for signal and power) as well as ventilation and crossflow convection cooling screens (for redundancy) whose openings would scale to shield the entire frequency of interest. Existing avionics and aircraft avionics cabinets can be retrofitted; the structural chassis walls may be replaced with the nanocomposite of the present invention. Alternatively, adhesive-backed, trim-to-fit, flexible nanocomposite panels of the present invention can be cut, formed, and bent to shape, then conductively bonded to existing chassis and cabinet walls. Or, broad-spectrum EMI/EMP shielding treatments may be applied directly onto prepared (and electrically grounded) conductive metal surfaces using a spray-on aerosol delivery system. The composite would be cured in situ after spraying.
(23) Note that in the specification and claims, about or approximately means within twenty percent (20%) of the numerical amount cited. As used herein, the singular forms a, an, and the include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to a functional group refers to one or more functional groups, and reference to the method includes reference to equivalent steps and methods that would be understood and appreciated by those skilled in the art, and so forth.
(24) Although the invention has been described in detail with particular reference to the disclosed embodiments, other embodiments can achieve the same results. Variations and modifications of the present invention will be obvious to those skilled in the art and it is intended to cover all such modifications and equivalents. The entire disclosures of all patents and publications cited above are hereby incorporated by reference.